- Open Access
- Total Downloads : 119
- Authors : Vikky Kumhar, Amit Sarda
- Paper ID : IJERTV6IS040407
- Volume & Issue : Volume 06, Issue 04 (April 2017)
- DOI : http://dx.doi.org/10.17577/IJERTV6IS040407
- Published (First Online): 15-04-2017
- ISSN (Online) : 2278-0181
- Publisher Name : IJERT
- License: This work is licensed under a Creative Commons Attribution 4.0 International License
Finite Element Analysis of Elbow Arthroplasty
Vikky Kumhar1*
Department of Mechanical Engineering, Christian College of Engineering and Technology, Bhilai, India
Amit Sarda2
Department of Mechanical Engineering, Christian College of Engineering and Technology, Bhilai, India
Abstract This article provides an information of the biomedical engineering modeling and approach of the elbow arthroplasty process. In this investigation also gives the conceptual design of the total replacement elbow joint which was allows the formulation and analyzing. The complete assembly of elbow model was designed in Creo parametric and analysis done using ANSYS tool, which was gives the results of proposed design and compare between existing and proposed work. Throughout the paper concluded the proposed design was gives the maximum efficient work in suitable material which is cobalt chromium alloys after analysis and comparison in good literature.
Keywords Elbow arthroplasty, finite element analysis, titanium, cobalt chromium, Von-Mises stresses.
*Corrosponding Author
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INTRODUCTION
The elbow implant is used on patients with arm joint pain and disabilities. Samples of conditions inflicting the arthritis and Rheumatoid Arthritis and Osteoarthritis. Arthritis could also be pathologic at intervals that the animal tissue settled in between the humerus and therefore the radius and ulna, that surrounds the joint becomes inflamed and thickened [1]. This may cause harm to the tissue and eventually, pain. Degenerative arthritis joint disease is most generally referred as "wear and tear" arthritis. This disorder happens due to repetitive movement of the joint, inflicting the animal tissue (cartilage) artefact the two bones forming the hinge movement to wear away. because of the animal tissue (cartilage) becomes dilatant, the humerus and radius and ulna would possibly rub against each other, inflicting pain to the elbow.
Figure 1 elbow implant X-ray images
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Link Segment Model
Link section analysis could also be started with a bottom level approach where ground reaction forces functioning on the feet is entered the model first or a top-down approach where forces
functioning on the hands area unit accustomed drive the analysis [3]. Link section models are of two types:
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Static link section model
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Dynamic link section model
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Link section model for the force analysis within the body once a load of specific amount is upraised within the bending condition [3]. The Figure 2 shows the detail link section model drawing of the physique in bend position.
Figure 2 Human body link segment model
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MATERIALS
For materials to be thought-about a biomaterial it ought to be ready to safely degree dependably replaces or perform in living tissue with an applicable physiological response [5]. In other words, the materials ought to be biocompatible. There are four teams of artificial biomaterials: polymers, metals, ceramics, and composites [5].
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Alumina
The single crystal corundum is hard and powerful but is simply too brittle to be used as articulating part. Like most ceramics, the strength of crystalline corundum is improved by decreasing consistency and grain size [5]. Aluminium oxide implant ought to have a flexural strength and modulus of elasticity of 380GPa to meet ASTM standards F603-78 [5].
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Stainless Steel
The most common form of stainless-steel used for implants is 316L (ASTM F138, F139) [7]. The inclusion of 2.25-3wt.% molybdenum improves salt water corrosion resistance, whereas the drop-in carbon content from 0.08-0.03wt.% maximum improves chloride resolution corrosion resistance.
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Cobalt-Chromium Alloys
The two cobalt-chromium alloys most often need to manufacture implants are CoCrMo (ASTM F75) and CoNiCrMo (ASTM F562). CoCrMo is castable and commonly used in implant applications, whereas CoNiCrMo is hot solid and regularly used to the stem of joint replacements in legs. The properties of CoCrMo ar usually improved by hot isostatic pressing [7]. The addition of chemical element provides the alloy higher strength by preventative grain growth. Despite these variations, however, the trade designation of Vitallium (or within the Great Britain, "Stellite") is often applied erroneously to every alloy. The cobalt-based alloys show a useful balance between mechanical properties and biocompatibility, every type being somewhat superior to stainless-steel in strength and corrosion resistance, however, dearer to manufacture.
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Titanium Alloys
Pure (98.9-99.6%) titanium has four completely different grades, correlating to an increase in impurity content [7]. These impurities, like oxygen, carbon, and nitrogen, greatly influence the mechanical properties of titanium through opening primary solid solution strengthening. Nitrogen offers
concerning double the strengthening impact per atom, however oxygen content varies the foremost between the grades, rising from 0.18% (grade 1) to 0.40% (grade 4). Hydrogen impurities will harm the malleability of the metallic element through the formation of hydrides [8]. Because of this, the most quantity of hydrogen allowed in titanium element is 0.015wt%. Cold working has been shown to increase the fatigue strength of titanium element [7]. The fatigue strength of pure titanium element is much inferior to alloyed titanium element, it is shown in Table 2.
TABLE 1 BLOOD COMPATIBILITY PROPERTIES OF BIOMATERIALS.
S.
No.
Properties
Stiffness
Strength
Corrosion resistance
Blood compatibil
ity
1.
Stainless steel
Best
Better
Good
Good
2.
Co-Cr alloys
Better
Good
Better
Better
3.
Ti-alloys
Good
Best
Best
Best
4.
Polyester
Good
High
High
Moderate
5.
Polytetrafluor
oethylene
High
High
High
Low
6.
Polyurethanes
Better
Medium
Medium
Good
TABLE 2 PROPERTIES OF IMPLANT MATERIALS.
Materials
ASTM
designation
Condition
Youngs modulus
(GPa)
Yield Strength
(MPa)
Tensile Strength
(MPa)
Fatigue endurance limit (at 107cycles, R=-1) (MPa)
Stainless Steel
F745
Annealed
190
221
483
221-280
F55, F56, F138, F139
Annealed
190
331
586
241-276
30% Cold worked
190
792
930
310-448
Cold forged
190
1213
1351
820
Co-Cr alloys
F75
As-cast/ Annealed 210
448-517
655-889
207-310
Powder metallurgy product, hot isostatically pressed
253
841
1277
725-950
F562
Hot forged
232
965-1000
1206
500
Cold worked, aged
232
1500
1795
689-793
(axial tension R = 0.05, 30 Hz)
Ti alloys
F67
30% Cold-Worked Grade 4
110
485
760
300
F136
Forged Annealed
116
896
965
620
Forged, heat treated
116
1034
1103
620-689
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METHODOLOGY
Elbow, vary of motion of an elbow joint is within the vary from full extension to full flexion. In this section, some mathematical model can be defined for elbow mechanism.
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Lever Mechanism in Human Body
Levers are one amongst the essential tools that were probably employed in prehistoric times. Levers were 1st diagrammatic concerning 260 BC by the standard Greek person Archimedes (287-212 BC). A lever could be a mechanical device that creates work easier for use; it involves moving a load around a pivot employing a force. Several of our basic tools use levers, together with scissors, pliers, hammer claws, nutcrackers, and tongs.
Their lever mechanism is classified into three class they are following [18]:
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The lever Class One, the pivot (fulcrum) is between the effort (force) and the weight.
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The Lever Class Second, the weight is between the pivot and the effort (force) and
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The Lever Class Three, the effort is between the pivot and the weight or load.
Figure 3 Free body diagram of elbow
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Equations of Arm Mechanism
From the free body diagram in Figure 5, several equations were derived to calculate all four forces to be put in finite element analysis. The derived equations were;
Moments about Elbow joint = 0,
——————(1)
are perpendicular measured distances from the elbow joint.
After the force acted by the biceps was calculated, the sum of the moment in the 'y-axis' direction will be taken as zero.
Sum of moments on 'y-axis' = 0,
——————-(2)
G is the weight of the forearm with an account of the gravitational force, acting vertically downwards. B is the force acted by the biceps, W is the weight of the object and R is the reaction force of the joint.
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Modelling and Analysis
The models have created in Creo Parametric software tool. Figure 4 has been shows that the existing modeling, proposed model has been modeled by changing existing design and surface geometry of model from sharp edge to smooth edges as shown in Figure 5.
Figure 4 Total replacement joint existing model
Figure 5 Total replacement joint proposed model
Figure 6 Meshing view of proposed model
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Boundary Conditions
All four forces were calculated and compiled for boundary conditions as shown in TABLE 3, shows the forces applied for all three materials [21].
TABLE 3 FORCES APPLIED TO THE ALL MATERIALS ELBOW MODAL [21].
Conditions
Force, N
G
W
B
R
0.1kg,
6.867
0.981
50.458
34.762
0.1kg,
6.867
0.981
25.229
17.381
0.1kg,
6.867
0.981
32.934
22689
0.5kg,
6.867
4.905
95.309
71765
0.5kg,
6.867
4.905
47.654
35.882
0.5kg,
6.867
4.905
62.209
46.481
1.5kg,
6.867
14.715
207.437
164273
1.5kg,
6.867
14.715
103.719
82137
1.5kg,
6.867
14.715
135.395
107.222
2.5kg,
6.867
24.525
319.566
256.391
2.5kg,
6.867
24.525
159.783
128.391
2.5g,
6.867
24.525
208.582
167.602
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RESULTS AND DISCUSSIONS
For this investigation, the criterions were viewed from the ANSYS 16.2, that are gives the Equivalent (von-Mises) Stress and a Principal Stress as shown in Figure 7 & 8. The various results from ANSYS 16.2 exploitation whole completely different cases.
(a) (b)
(c) (d)
Figure 7 Von-Mises Stress in proposed elbow joint for different materials (a)
Copper (B) Stainless Steel (c) Titanium and (d) Cobalt chromium alloy
(a) (b)
(c) (d)
Figure 8 Von-Mises Stress in proposed elbow joint for different materials (a) Copper (B) Stainless Steel (c) Titanium and (d) Cobalt chromium alloy
TABLE 4 RESULT OF VON-MISES STRESS FOR EXISTING MODEL
The Table 4 indicates that the validation results between existing and Khoo et. al., work.
Figure 9 Comparison of von mises stress between existing model and proposed model for all materials
Figure 10 Comparison max principal stress between existing model and proposed model for all materials
Figure 9 and 10, shows a comparison between existing model and proposed model for the different materials, such as copper, stainless steel, titanium and cobalt chromium. Proposed model gives 12.477% less von mises stress and 14.030% less maximum principal stress generation as compare to existing model respectively.
TABLE 5 COMPARISON BETWEEN EXISTING WORK WITH PROPOSED WORK
Stress
Titanium (Khoo et. al. (Existing
work)
Cobalt-Chromium with Proposed Model (Proposed work)
%
Difference
Von-Mises
42.365
37.079
12.477
Max
Principal
39.299
33.785
14.030
S. No.
Material
Khoo et. al. (Exist
Model)
Validation
% Error
1
Copper
45.755
45.1
1.4315
2
Stainless Steel
45.04
44.838
0.4485
3
Titanium
42.365
42.085
0.6609
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CONCLUSION
In this article, the applications of the biomaterial cobalt chromium metal for elbow arthroplasty implant has been proposed for higher performance. The proposed model performs the less von-mises stress generation as compare to existing implant. The comparisons of the each existing [7] and proposed model (present work) simulated results for identical environmental setups. Table 1, shown that relative differences between the commonly used metallic alloys or polymers as biomaterials, which clarify that the cobalt chromium has a better blood compatibility for the human body. The von mises and maximum principal stress percentage error between the existing work and the proposed work are 12.477% and 14.030% respectively is shown in Table 5, which is under design safe. Due to modification of design and surface conditions, the weight of proposed model was less as compare to existing and cost are also reduced, therefore the cobalt chromium is suitable for proposed design and existing design. By using cobalt chromium which will also result in a minimal principal stress on the implant.
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